View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 28537U 05004A 24278.90589670 0.00000600 00000-0 52087-3 0 05
2 28537 63.4004 216.3920 0497286 2.2610 357.7390 13.41038727 04
| Epoch (UTC): | 04 October 2024 21:44:29 |
| Eccentricity: | 0.0497286 |
| inclination: | 63.4004° |
| perigee height: | 733 km |
| apogee height: | 1477 km |
| right ascension of ascending node: | 216.3920° |
| argument of perigee: | 2.2610° |
| revolutions per day: | 13.41038727 |
| mean anomaly at epoch: | 357.7390° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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